Search filter

    • Year
      1906
      2018
    • Length
      12 m
      20 m
    • Height
      3 m
      6 m
    • Width
      1 m
      8 m
    • Diameter
      3 m
      9 m
    • Wing area
      96 m2
      144 m2
    • Wingspan (Beam)
      22 m
      34 m
    • Wing loading
      3 kg/m2
      829 kg/m2
    • Swept
      4 m
      10 m
    • Sweep
      25 deg
      68 deg
    • Aspect ratio
      1
      26
    • Disc area
      1 m2
      460 m2
    • Main rotor diameter
      1 m
      62 m
    • Rotor number
      1 qt
      8 qt
    • Blades per rotor
      4 qt
      5 qt
    • Disc loading
      17 kg/m2
      73 kg/m2
    • Tail rotor diameter
      0 m
      5 m
    • Empty weight
      4040 kg
      6060 kg
    • Max. takeoff weight (Gross weight)
      5640 kg
      8460 kg
    • Loaded weight
      5272 kg
      7908 kg
    • Crew
      3 per.
      5 per.
    • Useful load
      26 kg
      90700 kg
    • Payload
      23 kg
      122470 kg
    • Capacity passengers
      1 per.
      400 per.
    • Hardpoints
      1 qt
      2576 qt
    • Ground Speed
      158 km/h
      238 km/h
    • Max. Speed
      25 km/h
      28165 km/h
    • Сruise Speed
      132 km/h
      200 km/h
    • Stall Speed
      40 km/h
      258 km/h
    • Landing Speed
      68 km/h
      270 km/h
    • Minimum control speed
      24 km/h
      113 km/h
    • Never exceed speed
      107 km/h
      1050 km/h
    • Fuel Capacity
      23 l
      320000 l
    • Fuel External
      142 l
      10025 l
    • Power/mass
      0 hp/kg
      23 hp/kg
    • Thrust/weight
      0 kN/kg
      3 kN/kg
    • Afterburning thrust
      29 kN/kg
      980 kN/kg
    • Total Power
      1344 hp
      2016 hp
    • Thrust
      1 kN
      1914 kN
    • Service ceiling
      5200 m
      7800 m
    • Static ceiling
      3 m
      5485 m
    • Range (Ferry range)
      4 km
      40700 km
    • Range PTB (Ferry range)
      720 km
      10000 km
    • Сombat radius
      277 km
      7210 km
    • Endurance
      0 h
      150 h
    • Takeoff roll
      20 m
      3200 m
    • Landing roll
      20 m
      2570 m
    • Maximum glide ratio
      7
      43
    • Load factor from
      2 G
      9 G
    • Rate of climb
      196 m/min
      296 m/min
    • Rate of sink
      36 m/min
      56 m/min
    • Time to altitude
      0 min
      105 min
    • Propellers
      1 qt
      8 qt
    • Prop diameter
      1 m
      6 m
    • Prop blade number
      1 qt
      8 qt
    • Guns
      2 qt
      4 qt
    • Bombs
      1 qt
      250 qt
    • Missiles
      1 qt
      24 qt
    • Rockets
      1 qt
      76 qt
    • Torpedoes
      1 qt
      4 qt
    • Bombs weight
      2 kg
      39000 kg
    • Rockets weight
      1 kg
      48 kg
    • Number built
      0 qt
      2 qt
    • Price
      41 USD
      750000000 USD

Latécoère 6

TypeAircraft
Company

Groupe Latécoère

Scheme

Biplane

Geometry
Length (m)
1.9
 
16.0
88.7
Height (m)
0.6
 
4.7
50.1
Wings
Wing area (m2)
1.1
 
120
925
Wingspan (Beam) (m)
0.1
 
27.7
95
Weights
Empty weight (kg)
8
 
5,050
276,800
Max. takeoff weight (Gross weight) (kg)
154
 
7,050
575,000
Loaded weight (kg)
5
 
6,590
242,500
Capacity
Crew (per.)
1
 
4
112
Speeds
Ground Speed (km/h)
96.6
 
198
1,500
Сruise Speed (km/h)
52
 
166
3,087
Power
Total Power (hp)
0.4
 
1,680
60,000
4 powerplants 420 hp each
Performance
Service ceiling (m)
0.6
 
6,500
161,544
Dynamic Performance
Rate of climb (m/min)
1.9
 
246
36,000
Combat
Guns (qt)
1
 
3
18
7.7 mm (0.303 in) Lewis machine guns in dorsal, ventral and nose positions
Stat
Number built (qt)
0
 
1
43,000
Introduction 1924
First flight 01.06.1924

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